Proceedings of the 2nd International Conference on Advances in Mechanical Engineering and Industrial Informatics (AMEII 2016)

Double Terminal Sliding Mode Control of Airship Height Loop

Authors
YiDong Wang, Jinhuang Wu, Dingxiong Zhang, Hong Wang, Junwei Lei
Corresponding Author
YiDong Wang
Available Online April 2016.
DOI
10.2991/ameii-16.2016.290How to use a DOI?
Keywords
airship, pitch channel, adaptive, PID, stability
Abstract

A kind of double terminal sliding mode surface is constructed with a subsystem with a terminal sliding mode. This new strategy is proposed to solve the height control problem of a kind of airship system. And the main goal is to compute a ideal pitch angel such that the height of airship can trace the expected value. Also a Lyapunov stability theory is used to prove the whole system is stable. And at last, detailed simulation is done to testify the rightness of this method.

Copyright
© 2016, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 2nd International Conference on Advances in Mechanical Engineering and Industrial Informatics (AMEII 2016)
Series
Advances in Engineering Research
Publication Date
April 2016
ISBN
10.2991/ameii-16.2016.290
ISSN
2352-5401
DOI
10.2991/ameii-16.2016.290How to use a DOI?
Copyright
© 2016, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - YiDong Wang
AU  - Jinhuang Wu
AU  - Dingxiong Zhang
AU  - Hong Wang
AU  - Junwei Lei
PY  - 2016/04
DA  - 2016/04
TI  - Double Terminal Sliding Mode Control of Airship Height Loop
BT  - Proceedings of the 2nd International Conference on Advances in Mechanical Engineering and Industrial Informatics (AMEII 2016)
PB  - Atlantis Press
SN  - 2352-5401
UR  - https://doi.org/10.2991/ameii-16.2016.290
DO  - 10.2991/ameii-16.2016.290
ID  - Wang2016/04
ER  -